EP0419684A1 - Element de frottement dans un couple de frottement - Google Patents
Element de frottement dans un couple de frottement Download PDFInfo
- Publication number
- EP0419684A1 EP0419684A1 EP90906433A EP90906433A EP0419684A1 EP 0419684 A1 EP0419684 A1 EP 0419684A1 EP 90906433 A EP90906433 A EP 90906433A EP 90906433 A EP90906433 A EP 90906433A EP 0419684 A1 EP0419684 A1 EP 0419684A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- friction element
- friction
- element according
- zone
- frame
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
- 239000011159 matrix material Substances 0.000 claims abstract description 29
- 239000000463 material Substances 0.000 claims abstract description 26
- 230000007423 decrease Effects 0.000 claims abstract description 6
- 238000004804 winding Methods 0.000 claims description 7
- 230000008859 change Effects 0.000 claims description 2
- 241000264877 Hippospongia communis Species 0.000 abstract description 3
- 210000004027 cell Anatomy 0.000 description 17
- 239000012634 fragment Substances 0.000 description 8
- 230000035882 stress Effects 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 239000011248 coating agent Substances 0.000 description 5
- 238000000576 coating method Methods 0.000 description 5
- 238000004519 manufacturing process Methods 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 238000010276 construction Methods 0.000 description 4
- 230000006378 damage Effects 0.000 description 4
- 239000002783 friction material Substances 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 230000000694 effects Effects 0.000 description 3
- 230000017525 heat dissipation Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
- 230000008569 process Effects 0.000 description 3
- 230000000930 thermomechanical effect Effects 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000011324 bead Substances 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 229910001234 light alloy Inorganic materials 0.000 description 2
- 230000002787 reinforcement Effects 0.000 description 2
- 238000007493 shaping process Methods 0.000 description 2
- 229910000838 Al alloy Inorganic materials 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 239000002131 composite material Substances 0.000 description 1
- 230000021615 conjugation Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 238000013016 damping Methods 0.000 description 1
- 238000010410 dusting Methods 0.000 description 1
- 230000002349 favourable effect Effects 0.000 description 1
- 230000008642 heat stress Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 238000004806 packaging method and process Methods 0.000 description 1
- 230000008092 positive effect Effects 0.000 description 1
- 230000002028 premature Effects 0.000 description 1
- 230000009467 reduction Effects 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 210000002163 scaffold cell Anatomy 0.000 description 1
- 238000005245 sintering Methods 0.000 description 1
- 238000005728 strengthening Methods 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D69/02—Composition of linings ; Methods of manufacturing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D13/00—Friction clutches
- F16D13/58—Details
- F16D13/60—Clutching elements
- F16D13/64—Clutch-plates; Clutch-lamellae
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D13/00—Friction clutches
- F16D13/58—Details
- F16D13/72—Features relating to cooling
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/0006—Noise or vibration control
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D65/10—Drums for externally- or internally-engaging brakes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/02—Braking members; Mounting thereof
- F16D65/12—Discs; Drums for disc brakes
- F16D65/127—Discs; Drums for disc brakes characterised by properties of the disc surface; Discs lined with friction material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D65/00—Parts or details
- F16D65/78—Features relating to cooling
- F16D65/84—Features relating to cooling for disc brakes
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D2069/002—Combination of different friction materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D69/00—Friction linings; Attachment thereof; Selection of coacting friction substances or surfaces
- F16D2069/004—Profiled friction surfaces, e.g. grooves, dimples
Definitions
- the invention relates to friction pairings of machine parts and relates in particular to a friction element of a friction pairing.
- a friction disc (US, A, 3773153) which is made up of a composite, namely its outer parts are made of steel, but the core is made of corrugated aluminum plates.
- reinforcement sleeves leads to an increase in the cost of materials and the weight of the construction and, on the other hand, does not guarantee the optimum load-bearing capacity of the friction surface as well as the excess of the connection and the resistance to loosening, which in the end has a negative effect on the service life of the friction disc.
- a friction element of a friction pairing namely a brake disc
- SU a friction element of a friction pairing
- a brake disc which has a three-dimensional framework, which is accommodated in a matrix, which is made of a material with a high coefficient of thermal conductivity.
- Coating the friction surfaces of the disc from a wear-resistant material does not result in their optimal load-bearing capacity.
- the invention has for its object to provide such a friction element of a friction pair, the structure of which ensures a uniform resistance of different zones of the friction surface against destruction during operation while ensuring their optimal load-bearing capacity.
- a friction element of a friction pairing which contains a three-dimensional framework, which is accommodated in a matrix made of a material with a high coefficient of thermal conductivity, and a friction surface
- the framework is made of a wear-resistant material and at least in the zone of Arranged friction surface, which has a regular microrelief, which is formed by the matrix and the front end of the framework projecting above its surface.
- Such parts in the friction element according to the invention are the parts protruding over the matrix, and since they are arranged discretely and regularly on the friction surface, the latter proves to be one which essentially corresponds to the actual surface area of the contact surfaces. As a result, only a minimal amount of wear-resistant material is consumed, which has a positive effect on the cost of manufacturing the friction element.
- Such a design of the friction element also increases the overall rigidity and strength of the structure and reduces its mass.
- the friction surface of the friction element is partially formed by the matrix, which is made of a material with a high coefficient of thermal conductivity, the heat dissipation from the friction surface is improved, thereby increasing the useful life of the product as a whole.
- the scaffold can advantageously be designed in the form of a cell structure.
- the regular microrelief on the friction surface can preferably have a cell shape which contributes in the best way to increasing the working capacity and the service life of the friction element.
- Such an embodiment of the friction element can preferably be used as a brake drum of a motor vehicle, as a thrust bearing and the like.
- the area of the end face of the scaffolding projecting beyond the matrix decreases proportionally in the direction from the zone of the maximum load to the zone of the minimum load.
- the area of the end face can be changed by changing the cell size and / or the wall thickness of the cell structure and / or the arrangement density of the cells.
- the strengthening of the friction surface of the friction element in the zone of the maximum load which can be achieved due to the increased surface area of the end face of the frame, has the advantage that the wear of this zone slows down during operation. This creates the conditions for uniform wear of the friction surface, which experiences uneven thermomechanical stresses, which contributes to extending the useful life of the product.
- the framework of the friction element can preferably be made from a more wear-resistant material in the zone of the maximum load than in the zone of the minimum load.
- the micro-relief on one surface can preferably be configured differently from the regular micro-relief on the other surface in terms of configuration.
- Such training counteracts the occurrence of natural vibrations, a form of resonance of the wave, the clinking and beeping.
- Plates can preferably be arranged between the cells of the scaffold.
- the plates can also be used to prevent the above-mentioned shortcomings.
- the framework of the friction element is made from a corrugated band.
- the band must be wound in a helical line.
- Such a design prevents the possible packaging of the belts and thus contributes to the high-quality shaping of the friction element.
- the scaffold consists of at least two parts arranged in the same axis with rewinding in opposite directions.
- Such a design is very beneficial for the compensation of the axial component and the damping of the vibration and thus contributes to increasing the life of the friction element.
- the corrugated band must be wound up in a spiral shape with an incline that increases in the direction of increase in the radius of the spiral.
- Such a winding has the advantage that the friction material of the belts is arranged in accordance with the thermomechanical stresses acting on the friction surface, i.e. denser in the zone of maximum load of the product and less dense in the zone of minimum load, which favors a uniform resistance to destruction of the friction surface.
- corrugated band with an incline and a height which increases over its length in the direction of enlargement of the radius of the spiral serves the same purpose.
- the belts forming the framework can preferably be provided with corrugations.
- the corrugations enlarge the surface of the framework and increase its rigidity and strength.
- the perforation reinforces the anchor effect of the fastening of the bands in the matrix and improves the heat dissipation, which in the end increases the service life of the friction element.
- the winding direction of the spiral can preferably be with the direction of rotation of the friction element, e.g. a brake disc, so that compressive stresses act on them during operation.
- the friction element e.g. a brake disc
- Figure 1 shows a brake disc according to the invention.
- Figure 2 shows the brake disc in plan.
- FIG. 4 shows a scaffold in the form of a cell structure in axonometry
- FIG. 6 shows a fragment of a friction element, which illustrates the presence of a microrelief on the friction surface
- FIG. 10 shows a fragment of a friction element with a framework in the form of a spatial network in section
- FIG. 11 shows a brake disk with changing arrangement density of the cells of the frame on the friction surface in the plan view
- FIG. 13 shows a brake disc, on the mutually opposite friction surfaces of which the scaffold cells are designed in different configurations
- FIG. 14 shows the brake disc shown in FIG. 13 in a view from the left
- FIG. 15 shows the brake disc shown in FIG. 13 in a view from the right
- FIG. 16 shows a brake disc with a framework consisting of a corrugated band
- Figure 18 shows a scaffold made up of several pairs of tape windings which have an opposite winding direction
- Fig. 19 shows a scaffold which is designed in the form of a corrugated band which is wound into a flat spiral
- a friction element of a friction pairing contains a three-dimensional framework 1 (FIGS. 1, 2, 3, 4) which is accommodated in a matrix 2 made of a material with a high coefficient of thermal conductivity.
- the scaffold 1 can be in the form of honeycombs (Fig. 2, 4, 5), a grid (Fig. 7, 8), a spatial network (Fig. 9, 10) and the like made of a material that has a higher strength and heat wear resistance as the heat-dissipating material of the matrix 2, which fills this framework.
- the frame 1 can be made of steel and the matrix 2 of an aluminum alloy.
- the framework 1 and the matrix 2 are each made of alloys based on Mo, W and copper.
- the frame 1 has a coating (FIG. 3) which consists of a material which is compatible with the material of the frame 1 and the matrix 2 and has good thermal conductivity.
- Copper can preferably be used as the coating for the framework 1 based on Fe and for the matrix 2 based on Al.
- the scaffold 1 partially protrudes with its end face over the matrix 2 and, together with the latter, forms a friction surface 4 with discretely arranged sections of a wear-resistant material, via which contact occurs during the operation of the friction pairing.
- the frame 1 can be accommodated not only in the zone of the friction surface 4, but also in the entire volume of the friction element.
- the area of the part of the frame 1 on the friction surface 4 makes up from 3 to 70% in relation to the total friction surface 4, which corresponds to the actual contact surface area.
- the friction element can preferably be produced in the form of a reinforced casting.
- It can be shaped by sintering or dusting.
- the friction surface 4 is treated with the aim of giving it the final shape, the dimensions and the roughness.
- the friction surface 4 corresponds to a surface with a completely regular microrelief, for example with a hexagonal microrelief (FIGS. 2, 5, 6, 11, 12).
- an embodiment is most favorable in which the end face content of the scaffold 1 changes from the zone of the maximum load to the zone of the minimum load (FIGS. 2, 11, 12, 13, 14, 15, 19) proportionally reduced.
- the wear surface of the friction disks has a hyperbolic shape and that the deformation and wear decrease when the point of the conjugation surface is removed from the axis of rotation due to the reduction in pressure.
- the end face content of the scaffold 1 can be changed by changing the size of the cells 5 of the scaffold 1 and / or the thickness of its walls 6 and / or the arrangement density of the cells 5.
- each of them is reinforced by a framework 1 which has different configurations of the cells 5 (for example a square and a hexagonal) which have different contours of the regular microrelief ( 14, 15) form, or one additionally reinforces the friction surfaces 4 of the disk by plates 7 (FIG. 12), which are arranged radially distributed between the cells 5 of the frame 1, which eliminates vibrations.
- a framework 1 which has different configurations of the cells 5 (for example a square and a hexagonal) which have different contours of the regular microrelief ( 14, 15) form, or one additionally reinforces the friction surfaces 4 of the disk by plates 7 (FIG. 12), which are arranged radially distributed between the cells 5 of the frame 1, which eliminates vibrations.
- the framework 1 can be made of different materials with regard to the wear resistance. In the zone of maximum load, materials are to be used that have better physical and mechanical properties than in the zones of minimum load.
- the frame 1 can be made from a corrugated band 8 (FIG. 16).
- the corrugated band 8 is to be wound up helically, the turns of a flat band 9 being arranged between the turns of the spiral line.
- the bands 8, 9 are oriented with their end faces towards the friction surface 4 of the friction element, so that a regular microrelief is formed on the latter, the geometry of which is determined by the geometry of the cells 5 formed by the bands 8, 9.
- such a scaffold 1 is made of at least two parts arranged in the same axis with oppositely directed wind-up (FIGS. 17, 18).
- the corrugated band 8 is wound in a spiral line shape, the slope of the spiral increasing in the direction of enlargement of its radius (FIG. 19) in accordance with the arrangement of the load zones of the friction surface 4 and the slope and height of the beads along the length of the spiral in Increase the direction of enlargement of their radius.
- the winding direction of the spiral coincides with the direction of rotation of the friction element.
- turns of the corrugated band 9 are arranged.
- the strips 8, 9 are oriented with their end faces towards the friction surface 4, so that a microrelief is formed on the latter, the geometry of which is also determined by the geometry of the cells 5 formed by the strips 8, 9.
- the friction material is arranged on the friction surface 4 depending on its load character, namely more densely in the zone of the maximum load than in the zone of the minimum load.
- corrugations 11 are also provided on the surface of the belts 8, 9.
- the corrugations enlarge the surface of the reinforcement structure 1 and thus increase its rigidity and strength.
- the coating 3 of the framework 1 which has a high thermal conductivity and is well compatible with the heat-dissipating matrix material, favors this process because the coating 3 excludes the thermal barrier between the framework 1 and the matrix 2. As a result, the heat is distributed in the volume of the friction element.
- the friction element according to the invention is also suitable as a support structure, for example as a bearing sleeve with a friction surface which is designed and functions analogously to that described.
- the invention can be used in brake systems, in particular in passenger cars, in clutch disks, in various support structures and the like.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Braking Arrangements (AREA)
- Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
Abstract
Applications Claiming Priority (8)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU894672584A RU1775570C (ru) | 1989-04-04 | 1989-04-04 | Фрикционный элемент |
SU4672584 | 1989-04-04 | ||
SU4716748 | 1989-07-10 | ||
SU4716748 | 1989-07-10 | ||
SU4766345 | 1989-09-15 | ||
SU4766345 | 1989-09-15 | ||
SU4784102 | 1990-01-18 | ||
SU4784102 | 1990-01-18 |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0419684A1 true EP0419684A1 (fr) | 1991-04-03 |
EP0419684A4 EP0419684A4 (en) | 1991-10-02 |
Family
ID=27484929
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19900906433 Pending EP0419684A4 (en) | 1989-04-04 | 1990-04-04 | Friction element of a friction pair |
Country Status (5)
Country | Link |
---|---|
US (1) | US5163526A (fr) |
EP (1) | EP0419684A4 (fr) |
JP (1) | JPH03505249A (fr) |
HU (1) | HUT59209A (fr) |
WO (1) | WO1990012219A1 (fr) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0525439A1 (fr) * | 1991-07-29 | 1993-02-03 | Linde Aktiengesellschaft | Disque de frein |
WO1995001520A1 (fr) * | 1993-07-02 | 1995-01-12 | Knorr-Bremse Ag | Disque de frein pour freins a disque |
EP0687829A1 (fr) * | 1994-06-17 | 1995-12-20 | Wagner Electric Corporation | Matériau de friction renforcé |
WO2000032335A1 (fr) * | 1998-12-03 | 2000-06-08 | Otto Junker Gmbh | Piece moulee composite et son procede de fabrication |
CN109404432A (zh) * | 2018-12-28 | 2019-03-01 | 东北大学 | 一种金属挠性膜盘联轴节 |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2211928T3 (es) * | 1995-11-24 | 2004-07-16 | Deutsches Zentrum Fur Luft- Und Raumfahrt E.V | Disco de freno. |
US5680921A (en) * | 1996-02-07 | 1997-10-28 | Borg-Warner Automotive, Inc. | Transmission band assembly |
DE19622520C1 (de) * | 1996-06-05 | 1997-11-27 | Ebern Fahrzeugtech Gmbh | Innenbacken-Trommelbremse |
ATE215189T1 (de) * | 1996-12-13 | 2002-04-15 | Tmd Friction Gmbh | Teilbelagscheibenbremse und bremsbacke |
US5979615A (en) * | 1997-11-06 | 1999-11-09 | Otis Elevator Company | Carbon--carbon composite elevator safety brakes |
US6371261B1 (en) | 1997-11-06 | 2002-04-16 | Otis Elevator Company | Molybdenum alloy elevator safety brakes |
WO1999028646A2 (fr) * | 1997-11-27 | 1999-06-10 | Continental Teves Ag & Co. Ohg | Disque de frein, notamment pour vehicules automobiles |
EP1418065A1 (fr) * | 2002-11-06 | 2004-05-12 | ISCA S.p.A | Roue avec face de frottement en matériau à haut coéfficient de friction |
DE10324186A1 (de) * | 2003-05-28 | 2004-12-16 | Volkswagen Ag | Bremsscheibe für ein Fahrzeug |
US8978842B2 (en) * | 2011-11-24 | 2015-03-17 | Shimano Inc. | Bicycle disc brake rotor |
CN102853012B (zh) * | 2012-09-04 | 2015-12-09 | 浙江大学宁波理工学院 | 一种具有仿生结构的刹车片及其制备方法 |
CN105349097B (zh) * | 2015-12-10 | 2018-04-27 | 吉林大学 | 一种结构仿生摩擦材料及其制造方法 |
US9982730B2 (en) * | 2016-06-21 | 2018-05-29 | Nissan North America, Inc. | Brake pad |
US9982729B2 (en) * | 2016-06-21 | 2018-05-29 | Nissan North America, Inc. | Brake pad |
CN108386465A (zh) * | 2018-05-07 | 2018-08-10 | 安徽工业大学 | 一种具有仿生表面的汽车制动盘 |
DE102019205570A1 (de) * | 2019-04-17 | 2020-10-22 | Zf Friedrichshafen Ag | Kühlölleitelement sowie Antriebsstrang mit diesem |
CN111177846B (zh) * | 2019-12-11 | 2021-03-09 | 上海卫星工程研究所 | 快速创建大型蜂窝板内埋框架的三维建模方法 |
AT17380U1 (de) * | 2021-02-10 | 2022-02-15 | Plansee Se | Bremsscheibe für eine scheibenbremse |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1916387A (en) * | 1932-01-04 | 1933-07-04 | American Brake Shoe & Foundry | Brake shoe reenforce |
US1919168A (en) * | 1932-02-24 | 1933-07-18 | Evalena L Austin | Composite friction material and method for making the same |
US2747701A (en) * | 1950-12-07 | 1956-05-29 | Westinghouse Air Brake Co | Brake lining with wire reinforcement |
CH337038A (de) * | 1954-08-04 | 1959-03-15 | Goodyear Tire & Rubber | Verfahren zum Ableiten der Wärme, die bei der Vernichtung von kinetischer Energie entsteht, und Einrichtung zur Ausübung dieses Verfahrens |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB888444A (en) * | 1959-06-15 | 1962-01-31 | Eaton Mfg Co | Friction element for clutch or brake |
US3429766A (en) * | 1965-10-21 | 1969-02-25 | Raybestos Manhattan Inc | Clutch facing |
FR2168662A5 (fr) * | 1972-01-19 | 1973-08-31 | Skf Cie Applic Mecanique | |
US3773153A (en) * | 1972-01-26 | 1973-11-20 | Borg Warner | Rotor for clutch or brake |
US3841949A (en) * | 1972-10-25 | 1974-10-15 | Twin Disc Inc | Composite friction plate |
US4042085A (en) * | 1975-01-27 | 1977-08-16 | Caterpillar Tractor Co. | Friction coupling |
US4187932A (en) * | 1978-02-01 | 1980-02-12 | Goodyear Aerospace Corporation | Ribbon-wrapped carbon brake disk |
US4278153A (en) * | 1978-11-24 | 1981-07-14 | Goodyear Aerospace Corporation | Brake friction material with reinforcement material |
SU846875A2 (ru) * | 1979-01-25 | 1981-07-15 | Ивано-Франковский Институт Нефти И Газа | Тормозной диск |
SU893587A1 (ru) * | 1980-04-24 | 1981-12-30 | Предприятие П/Я Р-6601 | Трехслойна панель переменной жесткости |
SU921876A1 (ru) * | 1980-06-20 | 1982-04-23 | Институт Механики Полимеров Ан Латвсср | Армированный криогенный изол ционный материал |
SU1038260A1 (ru) * | 1981-10-28 | 1983-08-30 | Sojkin Boris M | Многослойна панель |
US4501347A (en) * | 1982-09-15 | 1985-02-26 | Abex Corporation | Segmented disc brake pad |
DE3527577A1 (de) * | 1985-08-01 | 1987-02-05 | Bergische Stahlindustrie | Bremsscheibe fuer niedrige antriebsleistung |
US4995500A (en) * | 1986-09-16 | 1991-02-26 | Borg-Warner Corporation | Groove pattern for high thermal capacity wet clutch |
SU1516647A1 (ru) * | 1986-12-08 | 1989-10-23 | Рыбинский Авиационный Технологический Институт | Тормозной диск |
JPH0242837A (ja) * | 1988-08-02 | 1990-02-13 | Fujitsu Ltd | 制御データ出力方式 |
-
1990
- 1990-04-04 EP EP19900906433 patent/EP0419684A4/de active Pending
- 1990-04-04 JP JP2506400A patent/JPH03505249A/ja active Pending
- 1990-04-04 HU HU903411A patent/HUT59209A/hu unknown
- 1990-04-04 US US07/613,855 patent/US5163526A/en not_active Expired - Fee Related
- 1990-04-04 WO PCT/SU1990/000085 patent/WO1990012219A1/fr not_active Application Discontinuation
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
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US1916387A (en) * | 1932-01-04 | 1933-07-04 | American Brake Shoe & Foundry | Brake shoe reenforce |
US1919168A (en) * | 1932-02-24 | 1933-07-18 | Evalena L Austin | Composite friction material and method for making the same |
US2747701A (en) * | 1950-12-07 | 1956-05-29 | Westinghouse Air Brake Co | Brake lining with wire reinforcement |
CH337038A (de) * | 1954-08-04 | 1959-03-15 | Goodyear Tire & Rubber | Verfahren zum Ableiten der Wärme, die bei der Vernichtung von kinetischer Energie entsteht, und Einrichtung zur Ausübung dieses Verfahrens |
Non-Patent Citations (1)
Title |
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See also references of WO9012219A1 * |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0525439A1 (fr) * | 1991-07-29 | 1993-02-03 | Linde Aktiengesellschaft | Disque de frein |
WO1995001520A1 (fr) * | 1993-07-02 | 1995-01-12 | Knorr-Bremse Ag | Disque de frein pour freins a disque |
EP0687829A1 (fr) * | 1994-06-17 | 1995-12-20 | Wagner Electric Corporation | Matériau de friction renforcé |
KR100323798B1 (ko) * | 1994-06-17 | 2002-07-02 | 다이안 케이.슈마허 | 보강된마찰재와그제조방법 |
WO2000032335A1 (fr) * | 1998-12-03 | 2000-06-08 | Otto Junker Gmbh | Piece moulee composite et son procede de fabrication |
CN109404432A (zh) * | 2018-12-28 | 2019-03-01 | 东北大学 | 一种金属挠性膜盘联轴节 |
Also Published As
Publication number | Publication date |
---|---|
HU903411D0 (en) | 1991-08-28 |
JPH03505249A (ja) | 1991-11-14 |
US5163526A (en) | 1992-11-17 |
HUT59209A (en) | 1992-04-28 |
EP0419684A4 (en) | 1991-10-02 |
WO1990012219A1 (fr) | 1990-10-18 |
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